4-internal forces beams _1 model (1)
TRANSCRIPT
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S t r u c t u r a l A n a l y s i s I )
INTERNAL FORCES BEAMS
PART ( 4 )
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. #
. #
#
. #
. #
. #
INTERNAL FORCES
(M @ sec = F *dF)
@M@
PART (4)
2014
2014
4/1
Structural Analysis (I) Internal Forces/BEAMS
P
Section Member
Normal Force (N)
Shear Force (Q)
Bending Moment (M)
P
R1 R2 R2R1
Loads
Reactions
N
M
Q
. #
Normal Force Diagram (N.F.D)
Shear Force Diagram (S.F.D)Bending Moment Diagram (B.M.D)
#
Normal Force (N)
Shear Force (Q)
Bending Moment (M)
N
NPOSITIVE NORMAL FORCE
N
N
NN
N
NNEGATIVE NORMAL FORCECOMPRESSION
POSITIVE SHEAR FORCE
NEGATIVE SHEAR FORCE
Q
Q
Q
QQ
Q
Q
Q
POSITIVE BENDING MOMENT
M
TENSION
MMM
+ve
-ve
+ve
-ve
+ve-ve
-ve
+ve
Datum
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PART (4)
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2014
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Structural Analysis (I) Internal Forces/BEAMS
EX Calculate Internal Forces at shown Sections then Draw I.F. Diagrams.
SEC 1
N = -8t (comp)
3t
8t1
Q = +3t ()
M = +3(0) =0 t.m
SEC 2
N = -8t (comp)
Q = +3t ()M = +3(3) =9 t.m
2
3t
8tN1
Q1
SEC 3N = -8t +8 =0t
Q = +3t () - 6t () = - 3t()
M = +3(3) = 9 t.m
N2
Q22
3t
8t 8t
6t
3
M2
SEC 4
N = 0t
Q = -3t()M = +3(6) - 6(3) = 0 t.m
N3
Q38t
6t4
3t
8t
Start from Left @ point a
REACTIONS
M a= 0.0
FY= 0.0
FX= 0.0 Xa= 8t
Ya= 3t
Yb= 3t
MM
NEGATIVE BENDING MOMENT
MM
a
Ya
Xa b
Yb
M
1 2
3
4
5
a
Ya
Xa b
Yb3t 3t
8t
10t3
4
8t
6t
9t.m1
2 3
4 5 6
/
/
/
6
7
8
9
wt/m`
#
+ve
-ve
Q
N
Datum
Left Right
+ve Sign summary
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SEC 5
N = 0t
Q = -3t()
M = 0 + 9 = +9 t.m
N4
Q4
8t
6t
3t
8t9t.m 5
9t.m5
SEC 6
N = 0t
Q = -3t()M = 3*9-6*6+9=0 t.m
N5
Q5
CHECK Right part
3t
6
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PART (4)
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2014
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Structural Analysis (I) Internal Forces/BEAMS
DRAWING
I.F.
SEC 1 2 3 4 5 6N
Q
M
-8t -8t 0t 0t 0t 0t
+3t +3t -3t -3t -3t -3t
0t.m +9t.m +9t.m 0t.m 0t.m+9t.m
a b
3t
10t3
4
8t
6t
9t.m1
2 3
4 5 6
3t
8t
8t
-
3t
3t
P=6t
9t.m9t.m
N.F.D
S.F.D
B.M.D
1cm=8t
1cm=3t
1cm=9t.m
-
+
M=9t.m
NONE
N = 0t Q = -3t()M = 0.0 t.m
M4
11
3
3
N=8t3
2
N.F.D & S.F.D
8t
6t
3t
8t9t.m 6
#
(
)
-1Datum
(
)
-2B.M.D. ( ( ( ) -3N.F.D , S.F.D &B.M.DN, Q &M Drop
S.F.D
.
Left / Right
Left Right
Drawing against force directio
Tension
Compression
Left Right
Drawing with force direction
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STANDARD CASES
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PART (4)
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2014
4/4
Structural Analysis (I) Internal Forces/BEAMS
P
S.F.D
B.M.D
P
P*L
+
10t
S.F.D
B.M.D
10t
30t.m
+
5t
S.F.D
B.M.D
5t
10t.m
+
P
S.F.D
B.M.D
P
P*L
+
Case (1)
Case (2)
Case (3)
S.F.D
B.M.D
NONE
10t.m
10t.m
S.F.D
B.M.D
NONE
M
M
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8t
4t 4t
S.F.D
B.M.D
8*84 =16t.m
4t
4t-
+
6t
4t
S.F.D
B.M.D
6*2*46 =8t.m
-+
2t
4t
2t
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PART (4)
2014
2014
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Structural Analysis (I) Internal Forces/BEAMS
P
P2
P2
S.F.D
B.M.D
PL4
P/2
P/2-
+
Case (4)
Case (5)
Case (6)
P
PbL
S.F.D
B.M.D
PabL
-+
PaL
Pb/L
Pa/L
7t
S.F.D
B.M.D
-
+
7t 7t
7t
7t
7t
B.M.D
7*2=14t.m
P
S.F.D
B.M.D
-
+
P P
P
P
P
B.M.D
P*a P*a
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1t
10t.m
1t
S.F.D-
1t
5t.m
B.M.D
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PART (4)
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2014
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Structural Analysis (I) Internal Forces/BEAMS
Case (7)
5t
S.F.D
B.M.D
5*93 =15t.m
-+
5t 5t
5t
5t
5t
P
S.F.D
B.M.D
PL3
-+
P P
P
P
P
PL3
Case (8)
Case (9)
2t
12t.m
S.F.D-
2t
2*126 =4t.m
B.M.D
2t
4*126 =8t.m
ML
M
S.F.D-
ML
MaL
MbL
B.M.D
ML
PL
M
PL
S.F.D-
M2
M2
B.M.D
ML
5t.m
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PART (4)
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Structural Analysis (I) Internal Forces/BEAMS
S.F.D
B.M.D
wL2
+
wt/m`
wL
wL8
Case (10)
S.F.D
B.M.D
2*52=25t.m
+
2t/m`
2*5 =10t
wL8
Case (11)
2*82=8t
S.F.D
B.M.D
-
+
2t/m`
8t
8t
8t
16t.m
16t.m
wL2
S.F.D
B.M.D
-
+
wt/m`
wL2
wL2
wL2
wL8
wL8
S.F.D
#
-1
-2B.M.D
-3Maximum MomentZero Shear Q=0t
Parabola
2
1
3
w
wL16t
Distributed loads
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PART (4)
2014
2014
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Structural Analysis (I) Internal Forces/BEAMS
SOLVED EXAMPLES
Ex(2)
Ya
Xa0t
3t/m`
12t
6t
6t
Yb12t
0.0t N.F.D
M b= 0.0
Ya(6) - 12(4) + 6(2) = 0.0
FX= 0.0 Xa= 0.0 t
Ya= 6 t
REACTIONS
FY= 0.0 Yb= 12t
-
+ +S.F.D
6t
6t
6t12t
B.M.D
WL8=6m.t
12t.m
6t
6t 8t.m 5t4
3 3t
4t
Ex(1)
M b= 0.0
Ya(6) - 6(4) + +8 + 4(2) = 0.0
FX= 0.0 Xa= 3t
Ya= 1.33t
REACTIONS
FY= 0.0 Yb= 8.67t
Ya
Xa3t
1.33t 8.67t Yb
3t
N.F.D
1.33t
4.67t
4t S.F.D8.67t
6t
2.66t.m
6.68t.m
1.32t.m
8t.m
B.M.D
8t.m
2nd Par.
+
-
-
0t.m
Required Draw Internal Forces Diagrams (N.F.D , S.F.D & B.M.D).
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PART (4)
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2014
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Structural Analysis (I) Internal Forces/BEAMS
0.0t
3t/m`4t 4t
18t
FX= 0.0 Xa= 0t
Ya13t Yb13t
Xa0tREACTIONS
LOAD symmetry
Ya= Yb=18+4*2
2 = 13.0t N.F.D
S.F.D+ +
4t
9t4t
9t
WL8=13.5m.t
2nd Par.
Ex(3)
WL8=13.5m.t
--
B.M.D
8t.m 8t.m
4t
4t/m`
12t
12t
4t/m`
6t 6t
4t
6t 6t
10t
2t 2t
4t
- -
++
S.F.D
B.M.D
12t.m
12t.m
WL8=4.5m.t
WL8=4.5m.t
Ya
Xa
Yb
4t/m`
12t
12t
4t/m`
6t 6tEx(4)
M b= 0.0
Ya(6) + 6(8)-12 (4.5)+12(1.5)
FX= 0.0 Xa= 0.0 t
Ya= - 4t()
REACTIONS
FY= 0.0 Yb= 4t
+6(2) = 0.0
Anti-Symmetric load
Symmetric S.F.D
Anti-Symmetric B.M.D
Symmetric load
Anti-Symmetric
Symmetric B.M.D
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PART (4)
2014
2014
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Structural Analysis (I) Internal Forces/BEAMS
2nd Par.
PL4=6m.t
WL/8=24m.t
++
-+
-
10t
43
8t
6t3t/m`
Ya
Xa8t
Yb19t 23t
24t
6t6t
6t.m
Ex(5)
M b= 0.0
-Ya(12) + 6(14)+24 (8)+6(2) -6-6(1) =0
FX= 0.0 Xa= 8t
Ya= 23t
REACTIONS
FY= 0.0 Yb= (6+6+24+6)-23 = 19t
CHECK
M a= -6-6*13+19*12-6*10-24*4+6*2 =0 .......O.K.
10t
43
8t6t3t/m`
Ya
Xa8t
Yb19t 23t
24t
6t6t
6t.m
6t
13t
7t 6t
8t
17t
6t.m
12t.m
14t.m
12t.m
28t.m
23t
19t6t
S.F.D
B.M.D
N.F.D0.0t
INTERNAL FORCES
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2nd Par.
WL8=1m.t
++
-
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PART (4)
2014
2014
4/11
Structural Analysis (I) Internal Forces/BEAMS
Ex(6)
Yb 25t
5t10t2t/m`
Ya
Xa0t
10t
10t.m
M b= 0.0
Ya(8) - 10 -10*2 - 2*10 (3) + 5(2) =0
FX= 0.0 Xa= 0t
Ya= 10t
REACTIONS
FY= 0.0 Yb= (20+10+5)-10 = 25tCHECK
M a= 5*10-25*8+10*6+20*5-10 = 0 .......O.K.
4t 4t 4t
20t
25t
5t10t2t/m`
10t
10t.m
12t 4t 4t 4t
10t
2t
12t16t
9t5t
14t.m
24t.m
14t.m14t.m
WL8=4m.t
S.F.D
B.M.D
25t
INTERNAL FORCES
8t
10t.m
24t.m
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2nd Par.
+
- - -
--
N.F.D
S.F.D
B.M.D
B
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PART (4)
2014
2014
4/12
Structural Analysis (I) Internal Forces/BEAMS
Ex(7)
2t/m` 10t.m
11t
4t
5t
4t
45
15t
15t
RA
8t
4t
4t
B2t/m` 10t.m
11t
4t
5t
4t
15t
15t 8t
4t
4t
15t 15t
4t
4t
5t
1t
11t
4t
M b= 0.0
R cos45(8) - 4(10) - 8(6) - 10 -4(3) - 4(2) -4(1.5) = 0.0
FX= 0.0 Xb= 15-4 = 11 t FY= 0.0 Yb= (4+8+4+4)-15 = 5t
Check M a= -4*1.5-5*8+4*6+12*3-10-4*1 = 0.0 .....O.K.
R= 152 t
REACTIONS
4t.m
24t.m
14t.m
6t.m
6t.m6t.m
16t.m
WL8=4m.t WL8=1m.t
15t
4t
10t.m
INTERNAL FORCES
6t.m
6t.m
M @ j= 0
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2nd Par.
WL/8=16m.t
+ +-
-
-
N.F.D
S.F.D
B.M.D
++
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PART (4)
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2014
4/13
Structural Analysis (I) Internal Forces/BEAMS
Ex(8)
b
Yb
Xb
5t
3
4
3t
4t
3
45
cos = 35
sin = 45R
Rsin45
Rcos45
45
6t
16t
2t/m`
M b= 0.0
R cos45(8) - 4(10) - 16(4) + 6(1) = 0.0
FX= 0.0 Xb= 12.25+3 = 15.25 t
FY= 0.0 Yb= (6+16+4) - 12.25 = 13.75 t
Check M a= 6(9) - 13.75(8) + 16(4) - 4(2) = 0.0
a
12.25t13.75t
15.25t
R= 12.252 t
b3t
4t
45
6t
16t
2t/m`a
12.25t 13.75t
15.25t12.25t
3t
15.25t6t
6t
6t
7.75t
8.25t
4t
6t.m
6t.m
6t.m8t.m
REACTIONS
INTERNAL FORCES
6t.m
6t.m
6t.m
6t.m
6t.m
6t
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@M@
PART (4)
2014
2014
Structural Analysis (I) Internal Forces/BEAMS
Ex(9)2t8t
4t/m`16t16t
8t
= 8.0 tX B
YA = 20 t
- 4 -16(8) - 10(4) -8(1) -16(2) +8(1) + 2(2) = 0Y (10)A
Check
Draw N.F.D , S.F.D & B.M.DA
2nd Parabola
10t 8t
20t
4t
6t
22t
10t
2t
4t.m
44t.m
12t.m
44t.m
8t.m
52t.m
4t.m
2nd Parabola
2nd Parabola
WL8=8t.m
N.F.D
S.F.D
B.M.D
YB = (10+16+16+8+2)-20 = 32 t
20t
10t
2t8t
20t 32t
16t 16t 8t
8t
4t.m
YA
XB
YB
2012/2013Mid-Term
Exam
REACTIONS
INTERNAL FORCES
WL8=8t.m
10t
8t
+
+
-
+
-
-
4t/m` 4t/m`
FX= 0.0
M B = 0.0
FY= 0.0
M A = 2*12+24*9-32*10-8*1+10*6+16*2-4 =0.0 O.K.
44t.m52t.m
8t.m
4t/m`
#END PART (4)